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EP1234117B1 - Shockproof mechanism, in particular for use in space sector - Google Patents

Shockproof mechanism, in particular for use in space sector Download PDF

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Publication number
EP1234117B1
EP1234117B1 EP00971506A EP00971506A EP1234117B1 EP 1234117 B1 EP1234117 B1 EP 1234117B1 EP 00971506 A EP00971506 A EP 00971506A EP 00971506 A EP00971506 A EP 00971506A EP 1234117 B1 EP1234117 B1 EP 1234117B1
Authority
EP
European Patent Office
Prior art keywords
fact
melting point
low melting
piston
point material
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP00971506A
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German (de)
French (fr)
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EP1234117A1 (en
Inventor
Guy Valembois
Dominique Medus
Jean Baricos
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Etienne LaCroix Tous Artifices SA
Original Assignee
Etienne LaCroix Tous Artifices SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
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Publication date
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Publication of EP1234117A1 publication Critical patent/EP1234117A1/en
Application granted granted Critical
Publication of EP1234117B1 publication Critical patent/EP1234117B1/en
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Expired - Lifetime legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B15/00Fluid-actuated devices for displacing a member from one position to another; Gearing associated therewith
    • F15B15/19Pyrotechnical actuators
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/645Separators
    • B64G1/6455Pyrotechnics; Using heat
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B15/00Fluid-actuated devices for displacing a member from one position to another; Gearing associated therewith
    • F15B15/20Other details, e.g. assembly with regulating devices
    • F15B15/22Other details, e.g. assembly with regulating devices for accelerating or decelerating the stroke

Definitions

  • the present invention relates to the field of mechanisms actuated by a thermal effect.
  • the present invention finds in particular, but not exclusively, application in the space industry, for example on launchers or satellites, in particular in the form of shears, valves, cuts strap, etc ...
  • the means actuated by a known thermal effect in particular the known pyrotechnic means, offer great possibilities. They in particular have a high potential between energy supplied and mass on board, as well as high reliability.
  • Document EP-A-0 311 026 is known, moreover, a mechanism comprising a heating means for generating a shock absorbing function.
  • the regulation electric heating means is however expensive to implement.
  • the object of the present invention is to propose a new mechanism which does not have the aforementioned drawbacks.
  • the system illustrated in the appended FIG. 1 comprises essentially a structure consisting of two sets 100, 200 susceptible of relative displacement, a block 300 of metal at low point of fusion and a highly exothermic pyrotechnic composition 400.
  • the two sets 100, 200 are susceptible of relative translation along the central axis O-O of the structure.
  • the first set 100 is composed of three parts: a body 110, a stopper 130 and a ring 150.
  • the body 110 is generally cylindrical of revolution around the O-O axis. More specifically, the body 110 has a central internal channel 112 storied.
  • the channel 112 is divided, according to FIG. 1, into three sections 114, 116, 118, juxtaposed axially.
  • Section 118 having the largest internal diameter, adjacent to a first end of the assembly 100 is provided with a tapping 119 over part of its length.
  • the internal thread 119 is complementary to a thread 132 provided on the plug 130.
  • Section 114 with the smallest internal diameter is adjacent to the second, opposite end of the assembly 100.
  • This small section 114 is provided, on its internal surface, with an annular groove 115 designed to receive an O-ring seal 170 intended to ensure the seal between the two assemblies 100, 200.
  • Section 116 showing the internal diameter between the two sections 114, 118 mentioned above is located axially between these two above sections.
  • the plug 130 has the general shape of a disk extending perpendicular to the axis O-O. As previously stated, the plug 130 has a thread 132 complementary to the internal thread 119. Thus, the plug 130 can be screwed onto the first end of the body 110 to close it.
  • the plug 130 has a through axial channel 134, for example central. This channel 134 is intended to receive an initiator 180, for pyrotechnic composition 400, for example an initiator electric.
  • the plug 130 is preferably provided with structures, for example a series of offset holes 136, intended to facilitate training in rotation of the plug 130 to secure it to the body 110.
  • the second assembly 200 consists of a piston centered on the axis O-O. It is stepped on its outer surface.
  • the piston 200 is stepped in the form of three sections: 214, 216, 218.
  • Section 214 of smaller diameter is located at the level of the second end of the body 110. Its external diameter is complementary of the internal diameter of the section 114 of the body 110.
  • the annular seal 170 aforementioned is supported on this external surface to ensure the seal between the two sets 100 and 200.
  • the larger diameter section 218 of the piston 200 is located at the vicinity of the first end of the body 110.
  • the external diameter of this section 218 is between the internal diameter of the section 116 and the internal diameter of the section 118 of the body 110.
  • Section 216 of piston 200 is located axially between the two abovementioned sections 214, 218. It has an external diameter included between that of sections 114 and 116 of body 110.
  • the ring 150 is formed of two cylindrical sections 152, 156 centered around the axis O-O connected by a central ring 154 transverse to the O-O axis.
  • the cylindrical section 152 has an external diameter included between the internal diameter of section 118 of the body and the internal diameter of the intermediate section 116 of the body 110.
  • the internal diameter of this cylindrical section 152 is complementary to the external diameter of the large section 218 of the piston and rests against this large section.
  • This cylindrical section 152 is located between the recess 117 and the axial face internal of the plug 130.
  • the axial length of the cylindrical section 152 is as it is immobilized, pinched between the two aforementioned elements, when the plug 130 is assembled on the body 110.
  • the second section 156 of the ring 150 has a diameter external diameter smaller than the internal diameter of section 116 and a diameter internal complementary to the external diameter of section 216 of the piston 200. It is based on the latter.
  • the radial extension of the intermediate ring 154 on the inside of the cylindrical section 152 is equal to the radial extension of section 218 of the piston on the outside of section 216.
  • the ring 150 defines in combination with the piston 200 a chamber 310 housing a volume of metal at low melting point 300.
  • This chamber 310 is delimited radially on the outside by the cylindrical section 152 of the ring 150, radially on the inside by the wall of the piston constituting the intermediate section 216, axially on the side first end by the large section 218 of the piston and axially side second end by the intermediate ring 154 of the ring 150.
  • the piston 200 is also provided with a central blind chamber 220 which opens onto the first end of the piston, opposite the electric initiator 180 and which houses the pyrotechnic composition 400.
  • the operation of the pyromechanism illustrated in Figure 1 is essentially the following: before implementing the electric initiator 180, and initiation of the pyrotechnic composition 400, the brazing formed by the metal with low melting point 300 located at the interfaces between parts 156 and 216 and between parts 152 and 218, as well as the phase solid of this metal 300 located in the chamber 310 ensure a secure blocking and efficient structure by ensuring relative immobilization between the two sets 100 and 200, the ring 150 being immobilized relative to the body 110 and the plug 130. It will be noted that in this position, the small section 214 of the piston 200 can emerge at least partially on outside of set 100.
  • the supply of the electric initiator 180 allows the triggering of pyrotechnic composition 400 and from there a rapid rise in the temperature of the metal 300 suitable for ensuring its fusion in order to release the piston 200 compared to the set 100.
  • the gases resulting from the chemical reaction at level of pyrotechnic composition 400 cause an expansion of the chamber 220 and therefore a displacement of the piston 200 away from the plug 130 by translation along the axis O-O.
  • This displacement of the piston 200 causes a reduction in the volume of the chamber 310, therefore a transfer of the low melting metal 300, by rolling between adjacent surfaces ring 150 and piston 200, to generate a damper function of movement.
  • the solidification of the metal with a low melting point 300 then makes it possible, after reconstitution of the solder, the final blocking of the device in a new state in which the extension of the piston 200 on the outside of the body 100, at its second end, is greater than the initial state.
  • a low point metal rolling can be provided melting point 300 not at the interfaces defined between the ring 150 and the piston 200 but at the level of calibrated bores formed in the ring 150 or in the piston 200 delimiting the chamber 310.
  • Low melting metal 300 can be thermally isolated from the external environment in order to avoid any risk of melting of this metal 300 before use of pyrotechnic composition 400.
  • the body 110 and the plug 130 arranged on the outside of the chamber 310 are made of materials exhibiting poor heat conduction properties or thermally insulating, while the piston 200 whose wall forming the intermediate section 216 is inserted between the pyrotechnic composition 400 and the metal with a low melting point 300 is preferably produced in a material good thermal conductor.
  • the metal 300 must be chosen to present a higher melting or softening temperature ambient to ensure its merger only in the event of implementation of initiator 180.
  • a structure composed of two assemblies 100, 200 capable of relative translation along an axis O-O, a metal with a low melting point 300 and a pyrotechnic composition 400.
  • the low-melting metal 300 provides a immobilization between the two assemblies 100, 200.
  • the metal with low melting point 300 is liquefied and the gas developed by the pyrotechnic composition 400 requests the sets 100, 200 with relative displacement.
  • the structure is again immobilized after cooling of the metal 300.
  • the metal 300 is located in a chamber 310 defined between, on the one hand, a ring 150 immobilized between a body 110 and a plug 130, and on the other hand a piston 200. More again precisely, the chamber 310 is delimited by elements of the ring 150 and elements of the piston 200, generally in L having each an axial section and a radial section.
  • FIG. 2 presents with respect to Figure 1 a number of characteristic points, among which we may cite the following.
  • the piston 200 is formed of an annular structure which does not directly provide the actuator output effect, but controls the output element.
  • this output element is formed of a structure 230 can be formed for example of a nut, a clamp system made up of different segments, for example threads equi-distributed around the O-O axis, or any equivalent means.
  • This forming element output actuator 230 is trapped in the initial rest position between two truncated cones 219, 139 formed respectively on the piston 200 and on the cap 130.
  • the piston 200 is formed from two parts 202, 204 assembled by thread with an interposed seal 206.
  • An O-ring 170 is placed in a groove 203 in the part 202 to seal between the piston 200 and the body 110, so comparable to Figure 1.
  • An additional seal 172 placed in a groove 137 of the plug 130 seals between the latter and the piston 200.
  • the initiator 180 is placed in a radial passage opposite the axis O-O passing through the wall of the body 110.
  • the initiator 180 thus opens into an annular chamber 140 containing the pyrotechnic composition 400.
  • This chamber 140 is delimited radially on the outside by the wall internal of the body 110, axially on the second end of the system by a transverse surface of the piston 200 and axially on the first end and radially on the inside by the ring 150.
  • the body 110 has a flange 1102 directed radially inwards and comprising a sheath 1104 provided with an internal thread 1106.
  • Such thread 1106 can receive any additional threaded element in front be temporarily maintained in relation to an associated associated element meanwhile by the thread 232 of the central element 230 formed of a nut or pliers.
  • the device illustrated in FIG. 2 can find application in the controlled release, during the implementation of the initiator 180, of a assembly carried out by threaded elements engaged respectively with 1106 and 232 threads.
  • the liquid metal 400 is then laminated in the set of adjustments formed between the piston 200 and the ring 150, to form a damping function controlling the dynamics of the piston.
  • the first set 100 is formed by assembly of a body 110 and a plug 130.
  • the pyrotechnic initiator 180 is placed in a radial channel passing through the wall of the external body 110 and opens into a chamber annular 140 delimited by the body 110, the ring 150, and in its portion radially internal by the external periphery of the piston 200.
  • the ring 150 is also linked to the first set 100. It has for this a pinched portion between a shoulder of the body 110 and the cap 130.
  • the annular chamber 310 which contains the metal at low point fusion 300 forming solder, located radially on the inside of the chamber 140 and containing the pyrotechnic composition 400 is delimited by two pairs of L-shaped walls belonging respectively to the ring 150 and to the piston 200, each of these two pairs of walls having a wall 154, 218 of radial orientation transverse to the axis O-O and a wall 152, 216 axial orientation parallel to the O-O axis.
  • the chamber 140 containing the composition pyrotechnic 400 being delimited only radially on the inside by the piston 200, it is understood that the gases possibly generated by the pyrotechnic composition 400 cannot stress the structure in displacement.
  • the piston 200 is stressed at displacement towards the second end of the structure, after fusion of the solder 300 by an auxiliary biasing element, for example a spring.
  • the piston 200 can be stressed by an element outside the structure illustrated in FIG. 3, for example a strap biasing the piston 200 towards the outside of the body 110.
  • the illustrated embodiment in FIG. 3 makes it possible inter alia to cause a relaxation between the tensioned parts such as straps, cables, etc ...
  • the structure comprises two pyrotechnic compositions 400, 410 linked together by a pyrotechnic relay 420.
  • the first pyrotechnic composition 400 communicates with the electric initiator 180. It is placed in an annular chamber 220 formed in the piston 200 near the metal 300, more precisely radially on the inside of the chamber 310 delimited by the ring 150 and the outer periphery of the piston 200.
  • This first pyrotechnic composition 400 is strongly exothermic but can generate little gas if necessary. She has for function of melting the adjacent metal 300.
  • the second pyrotechnic composition 410 is placed in a blind chamber 222 formed in a central position in the piston 200 and leading to the first end of the cap side structure shutter 130.
  • the pyrotechnic delay 420 is placed in a passage radial connecting the two chambers 220, 222.
  • the second composition pyrotechnic 410 is implemented after the first composition pyrotechnic 400, according to a delay defined by the combustion of the delay pyrotechnic 420.
  • the second pyrotechnic composition 410 is designed to generate a sufficient volume of gas to move the piston 200 as previously described with reference to FIG. 1.
  • the variant of embodiment illustrated in Figure 5 also includes two compositions pyrotechnics 400, 410 intended respectively to ensure the fusion of metal 300 and the generation of clean gas to move the piston 200.
  • the two compositions pyrotechnics 400, 410 are not connected by a pyrotechnic delay.
  • they are associated with initiators, for example electrical, respective, 180, 182 carried by the plug 130.
  • the sequencing is not controlled by pyrotechnic effect due to a delay as described for figure 4, but by applying appropriate signals on the respective initiators 180, 182.
  • the first pyrotechnic composition 180 highly exothermic is located adjacent to metal 300, in an annular piston chamber 200, while the second pyrotechnic composition 410, generating gas, is located in a blind central chamber 222 of the piston 200.
  • the device according to the present invention essentially constitutes a linear displacement actuation according to the O-O axis of the device as a variant, provision can be made for the latter to generate forces transverse to the axis O-O, for example of clamp by tightening of segments of general axial orientation equi-distributed around the axis O-O, by means, in a corner or in a cone linked to the displaced piston 200.

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  • Fluid Mechanics (AREA)
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  • Chemical & Material Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
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  • Automotive Seat Belt Assembly (AREA)
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Abstract

The mechanism includes a low melting point material (300) such as paraffin or a eutectic alloy, at least one electric or highly exothermal pyrotechnical composition heater (400), and a device suitable for throttling the low melting point material (300) in the liquid state, after the heater is actuated, thus performing a shock-absorbing function. The device further includes at least two concentric surfaces (154, 216; 152, 218) defining, a set of clearances between them and provided respectively on ring and piston parts (150, 200) that are capable of moving in order to throttle the low melting point material (300) through the set of clearances defined between the concentric surfaces. - Before an electrical initiator (180) is used to initiate the pyrotechnical composition, the soldered connection constituted by the low melting point metal at the interfaces between a cylindrical part 156 and the middle diameter piston segment (216) and between the another cylindrical part 152 and the largest diameter piston segment (218), and also the solid phase of this metal situated inside the a chamber (310), provides reliable and effective blocking of the structure ensuring that two assemblies (100 and 200) are prevented from moving relative to each other, with a ring (150) being prevented from moving relative to a body (110) and to a plug (130). In this position, the small section (214) of the piston (200) can emerge at least in part to the outside of the assembly (100). When the electrical initiator (180) is powered, the pyrotechnical composition is triggered to rapidly raises the temperature of the metal to melt it, thereby releasing the piston relative to the assembly (100). The gas coming from the chemical reaction of the pyrotechnical composition causes the chamber (220) to expand and thus moves the piston away from the plug in translation along the axis O-O. This displacement of the piston reduces the volume of the chamber (310) and thus transfers the low melting point metal by throttling it between the adjacent surfaces of the ring (150) and of the piston, thus performing a damping function on the movement. The low melting point metal then re-solidifies to reconstitute the solder connection and finally block the device in a new state in which the piston extends further from the second end of the body (100) than it did in the initial state.

Description

La présente invention concerne le domaine des mécanismes actionnés par un effet thermique.The present invention relates to the field of mechanisms actuated by a thermal effect.

La présente invention trouve notamment, mais non exclusivement, application dans le domaine de l'industrie spatiale, par exemple sur les lanceurs ou les satellites, notamment sous forme de cisaille, vanne, coupe sangle, etc ...The present invention finds in particular, but not exclusively, application in the space industry, for example on launchers or satellites, in particular in the form of shears, valves, cuts strap, etc ...

Les moyens actionnés par un effet thermique connus, notamment les moyens pyrotechniques connus, offrent de grandes possibilités. Ils présentent en particulier un fort potentiel entre énergie fournie et masse embarquée, ainsi qu'une grande fiabilité.The means actuated by a known thermal effect, in particular the known pyrotechnic means, offer great possibilities. They in particular have a high potential between energy supplied and mass on board, as well as high reliability.

Cependant, ces mécanismes présentent également un inconvénient majeur : la grande dynamique induite par leur fonctionnement.However, these mechanisms also have a drawback major: the great dynamics induced by their functioning.

En effet, les niveaux de chocs et de vibrations sont souvent rédhibitoires à l'utilisation d'équipements fragiles à leur proximité.Indeed, the shock and vibration levels are often prohibitive to the use of fragile equipment near them.

Du document EP-A-0 311 026 est connu, par ailleurs, un mécanisme cmnportant un moyen de chauffage permettant de générer une fonction amortisseur de choc. La régulation du moyen de chauffage électrique est cependant coûteuse à mettre en oeuvre.Document EP-A-0 311 026 is known, moreover, a mechanism comprising a heating means for generating a shock absorbing function. The regulation electric heating means is however expensive to implement.

La présente invention a pour but de proposer un nouveau mécanisme qui ne présente pas les inconvénients précités.The object of the present invention is to propose a new mechanism which does not have the aforementioned drawbacks.

Ce but est atteint dans le cadre de la présente invention, grâce à un équipement conforme à la revendication 1 annexée, laquelle est délimitée sous forme d'un préambule et d'une partie caractérisante par rapport à EP-A-0 311 026. This object is achieved in the context of the present invention, thanks to a equipment according to claim 1 appended, which is delimited in the form of a preamble and of a characterizing part compared to EP-A-0 311 026.

D'autres caractéristiques, buts et avantages de la présente invention apparaítront à la lecture de la description détaillée qui va suivre et en regard des dessins annexés, donnés à titre d'exemples non limitatifs et sur lesquels :

  • la figure 1 représente schématiquement une structure conforme à la présente invention, sous forme d'un actionneur linéaire vue en coupe axiale partielle longitudinale, et
  • les figures 2 à 5 représentent quatre variantes de réalisation de mécanismes conformes à la présente invention.
Other characteristics, objects and advantages of the present invention will appear on reading the detailed description which follows and with reference to the appended drawings, given by way of nonlimiting examples and in which:
  • FIG. 1 schematically represents a structure in accordance with the present invention, in the form of a linear actuator seen in partial longitudinal axial section, and
  • Figures 2 to 5 show four alternative embodiments of mechanisms according to the present invention.

On va tout d'abord décrire la structure de l'actionneur linéaire illustré sur la figure 1 annexée.We will first describe the structure of the illustrated linear actuator in Figure 1 attached.

Le système illustré sur la figure 1 annexée comprend essentiellement une structure constituée de deux ensembles 100, 200 susceptibles de déplacement relatif, un bloc 300 de métal à bas point de fusion et une composition pyrotechnique 400 fortement exothermique.The system illustrated in the appended FIG. 1 comprises essentially a structure consisting of two sets 100, 200 susceptible of relative displacement, a block 300 of metal at low point of fusion and a highly exothermic pyrotechnic composition 400.

Dans le cas d'espèce, les deux ensembles 100, 200 sont susceptibles de translation relative selon l'axe central O-O de la structure.In the present case, the two sets 100, 200 are susceptible of relative translation along the central axis O-O of the structure.

Le premier ensemble 100 est composé de trois pièces : un corps 110, un bouchon 130 et une bague 150.The first set 100 is composed of three parts: a body 110, a stopper 130 and a ring 150.

Le corps 110 est généralement cylindrique de révolution autour de l'axe O-O. Plus précisément, le corps 110 possède un canal interne central 112 étagé. Le canal 112 est divisé, selon la figure 1, en trois sections 114, 116, 118, juxtaposées axialement.The body 110 is generally cylindrical of revolution around the O-O axis. More specifically, the body 110 has a central internal channel 112 storied. The channel 112 is divided, according to FIG. 1, into three sections 114, 116, 118, juxtaposed axially.

La section 118 présentant le diamètre interne le plus important, adjacente à une première extrémité de l'ensemble 100 est munie d'un taraudage 119 sur une partie de sa longueur. Le taraudage 119 est complémentaire d'un filetage 132 prévu sur le bouchon 130. Section 118 having the largest internal diameter, adjacent to a first end of the assembly 100 is provided with a tapping 119 over part of its length. The internal thread 119 is complementary to a thread 132 provided on the plug 130.

La section 114 présentant le plus petit diamètre inteme est adjacente à la seconde extrémité, opposée, de l'ensemble 100. Cette petite section 114 est munie, sur sa surface interne, d'une gorge annulaire 115 conçue pour recevoir un joint torique d'étanchéité 170 destiné à assurer l'étanchéité entre les deux ensembles 100, 200.Section 114 with the smallest internal diameter is adjacent to the second, opposite end of the assembly 100. This small section 114 is provided, on its internal surface, with an annular groove 115 designed to receive an O-ring seal 170 intended to ensure the seal between the two assemblies 100, 200.

La section 116 présentant le diamètre interne intermédiaire entre les deux sections 114, 118 précitées est située axialement entre ces deux sections précitées.Section 116 showing the internal diameter between the two sections 114, 118 mentioned above is located axially between these two above sections.

Le bouchon 130 a la forme générale d'un disque s'étendant perpendiculairement à l'axe O-O. Comme indiqué précédemment, le bouchon 130 possède un filetage 132 complémentaire du taraudage 119. Ainsi, le bouchon 130 peut être vissé sur la première extrémité du corps 110 pour obturer celle-ci. Le bouchon 130 possède un canal axial traversant 134, par exemple central. Ce canal 134 est destiné à recevoir un initiateur 180, pour la composition pyrotechnique 400, par exemple un initiateur électrique.The plug 130 has the general shape of a disk extending perpendicular to the axis O-O. As previously stated, the plug 130 has a thread 132 complementary to the internal thread 119. Thus, the plug 130 can be screwed onto the first end of the body 110 to close it. The plug 130 has a through axial channel 134, for example central. This channel 134 is intended to receive an initiator 180, for pyrotechnic composition 400, for example an initiator electric.

Le bouchon 130 est de préférence muni de structures, par exemple une série de perçages excentrés 136, destinés à faciliter l'entraínement à rotation du bouchon 130 pour assurer sa fixation sur le corps 110.The plug 130 is preferably provided with structures, for example a series of offset holes 136, intended to facilitate training in rotation of the plug 130 to secure it to the body 110.

Il est défini au niveau de la zone de liaison entre la section 118 de plus grande dimension et la section intermédiaire 116, un décrochement 117 sous forme d'une couronne annulaire transversale à l'axe O-O, dirigé vers la première extrémité de l'ensemble 100.It is defined at the level of the connection zone between section 118 of larger dimension and the intermediate section 116, a step 117 in the form of an annular crown transverse to the axis O-O, directed towards the first end of the assembly 100.

Selon le mode de réalisation illustré sur la figure 1, le second ensemble 200 est constitué d'un piston centré sur l'axe O-O. Celui-ci est étagé sur sa surface externe.According to the embodiment illustrated in Figure 1, the second assembly 200 consists of a piston centered on the axis O-O. It is stepped on its outer surface.

Plus précisément encore, selon le mode de réalisation illustré sur la figure 1, le piston 200 est étagé sous forme de trois sections : 214, 216, 218.More precisely still, according to the embodiment illustrated on the FIG. 1, the piston 200 is stepped in the form of three sections: 214, 216, 218.

La section 214 de plus petit diamètre est située au niveau de la seconde extrémité du corps 110. Son diamètre externe est complémentaire du diamètre interne de la section 114 du corps 110. Le joint annulaire 170 précité prend appui sur cette surface externe pour assurer l'étanchéité entre les deux ensembles 100 et 200.Section 214 of smaller diameter is located at the level of the second end of the body 110. Its external diameter is complementary of the internal diameter of the section 114 of the body 110. The annular seal 170 aforementioned is supported on this external surface to ensure the seal between the two sets 100 and 200.

La section 218 de plus grand diamètre du piston 200 est située au voisinage de la première extrémité du corps 110. Le diamètre externe de cette section 218 est compris entre le diamètre interne de la section 116 et le diamètre interne de la section 118 du corps 110.The larger diameter section 218 of the piston 200 is located at the vicinity of the first end of the body 110. The external diameter of this section 218 is between the internal diameter of the section 116 and the internal diameter of the section 118 of the body 110.

La section 216 du piston 200 est située axialement entre les deux sections précitées 214, 218. Elle possède un diamètre externe compris entre celui des sections 114 et 116 du corps 110.Section 216 of piston 200 is located axially between the two abovementioned sections 214, 218. It has an external diameter included between that of sections 114 and 116 of body 110.

La bague 150 est formée de deux tronçons cylindriques 152, 156 centrés autour de l'axe O-O reliés par un anneau central 154 transversal à l'axe O-O.The ring 150 is formed of two cylindrical sections 152, 156 centered around the axis O-O connected by a central ring 154 transverse to the O-O axis.

Le tronçon cylindrique 152 possède un diamètre externe compris entre le diamètre interne de la section 118 du corps et le diamètre interne de la section intermédiaire 116 du corps 110. Le diamètre interne de ce tronçon cylindrique 152 est complémentaire du diamètre externe de la grande section 218 du piston et repose contre cette grande section. Ce tronçon cylindrique 152 est situé entre le décrochement 117 et la face axiale interne du bouchon 130. La longueur axiale du tronçon cylindrique 152 est telle que celui-ci est immobilisé, pincé entre les deux éléments précités, lorsque le bouchon 130 est assemblé sur le corps 110.The cylindrical section 152 has an external diameter included between the internal diameter of section 118 of the body and the internal diameter of the intermediate section 116 of the body 110. The internal diameter of this cylindrical section 152 is complementary to the external diameter of the large section 218 of the piston and rests against this large section. This cylindrical section 152 is located between the recess 117 and the axial face internal of the plug 130. The axial length of the cylindrical section 152 is as it is immobilized, pinched between the two aforementioned elements, when the plug 130 is assembled on the body 110.

Le second tronçon 156 de la bague 150 possède un diamètre externe inférieur au diamètre interne de la section 116 et un diamètre interne complémentaire du diamètre externe de la section 216 du piston 200. II repose sur ce dernier.The second section 156 of the ring 150 has a diameter external diameter smaller than the internal diameter of section 116 and a diameter internal complementary to the external diameter of section 216 of the piston 200. It is based on the latter.

L'extension radiale de l'anneau intermédiaire 154 sur l'intérieur du tronçon cylindrique 152 est égale à l'extension radiale du tronçon 218 du piston sur l'extérieur de la section 216.The radial extension of the intermediate ring 154 on the inside of the cylindrical section 152 is equal to the radial extension of section 218 of the piston on the outside of section 216.

Ainsi, la bague 150 définit en combinaison avec le piston 200 une chambre 310 logeant un volume de métal à bas point de fusion 300.Thus, the ring 150 defines in combination with the piston 200 a chamber 310 housing a volume of metal at low melting point 300.

Cette chambre 310 est délimitée radialement sur l'extérieur par le tronçon cylindrique 152 de la bague 150, radialement sur l'intérieur par la paroi du piston constituant la section intermédiaire 216, axialement côté première extrémité par la grande section 218 du piston et axialement côté seconde extrémité par l'anneau intermédiaire 154 de la bague 150.This chamber 310 is delimited radially on the outside by the cylindrical section 152 of the ring 150, radially on the inside by the wall of the piston constituting the intermediate section 216, axially on the side first end by the large section 218 of the piston and axially side second end by the intermediate ring 154 of the ring 150.

Le piston 200 est par ailleurs muni d'une chambre borgne centrale 220 qui débouche sur la première extrémité du piston, en regard de l'initiateur électrique 180 et qui loge la composition pyrotechnique 400.The piston 200 is also provided with a central blind chamber 220 which opens onto the first end of the piston, opposite the electric initiator 180 and which houses the pyrotechnic composition 400.

Le fonctionnement du pyromécanisme illustré sur la figure 1 est pour l'essentiel le suivant : avant mise en oeuvre de l'initiateur électrique 180, et initiation de la composition pyrotechnique 400, la brasure constituée par le métal à bas point de fusion 300 situé au niveau des interfaces entre les pièces 156 et 216 et entre les pièces 152 et 218, ainsi que la phase solide de ce métal 300 situé dans la chambre 310 assurent un blocage sûre et efficace de la structure en assurant une immobilisation relative entre les deux ensembles 100 et 200, la bague 150 étant immobilisée par rapport au corps 110 et au bouchon 130. On notera que dans cette position, la petite section 214 du piston 200 peut émerger au moins partiellement sur l'extérieur de l'ensemble 100.The operation of the pyromechanism illustrated in Figure 1 is essentially the following: before implementing the electric initiator 180, and initiation of the pyrotechnic composition 400, the brazing formed by the metal with low melting point 300 located at the interfaces between parts 156 and 216 and between parts 152 and 218, as well as the phase solid of this metal 300 located in the chamber 310 ensure a secure blocking and efficient structure by ensuring relative immobilization between the two sets 100 and 200, the ring 150 being immobilized relative to the body 110 and the plug 130. It will be noted that in this position, the small section 214 of the piston 200 can emerge at least partially on outside of set 100.

L'alimentation de l'initiateur électrique 180 permet le déclenchement de la composition pyrotechnique 400 et de là une élévation rapide de la température du métal 300 propre à assurer sa fusion afin de libérer le piston 200 par rapport à l'ensemble 100. Les gaz issus de la réaction chimique au niveau de la composition pyrotechnique 400 provoquent une expansion de la chambre 220 et donc un déplacement du piston 200 en éloignement du bouchon 130 par translation selon l'axe O-O. Ce déplacement du piston 200 entraíne une réduction du volume de la chambre 310, donc un transfert du métal à bas point de fusion 300, par laminage entre les surfaces adjacentes de la bague 150 et du piston 200, pour générer une fonction d'amortisseur de mouvement.The supply of the electric initiator 180 allows the triggering of pyrotechnic composition 400 and from there a rapid rise in the temperature of the metal 300 suitable for ensuring its fusion in order to release the piston 200 compared to the set 100. The gases resulting from the chemical reaction at level of pyrotechnic composition 400 cause an expansion of the chamber 220 and therefore a displacement of the piston 200 away from the plug 130 by translation along the axis O-O. This displacement of the piston 200 causes a reduction in the volume of the chamber 310, therefore a transfer of the low melting metal 300, by rolling between adjacent surfaces ring 150 and piston 200, to generate a damper function of movement.

La solidification du métal à bas point de fusion 300 permet ensuite, après reconstitution de la brasure, le blocage définitif du dispositif dans un nouvel état dans lequel l'extension du piston 200 sur l'extérieur du corps 100, au niveau de sa seconde extrémité, est supérieure à l'état initial.The solidification of the metal with a low melting point 300 then makes it possible, after reconstitution of the solder, the final blocking of the device in a new state in which the extension of the piston 200 on the outside of the body 100, at its second end, is greater than the initial state.

L'homme de l'art comprendra aisément qu'un tel pyromécanisme constitue un actionneur linéaire avantageux. Those skilled in the art will readily understand that such a pyromechanism constitutes an advantageous linear actuator.

Bien entendu, différentes variantes de réalisation du dispositif ainsi décrit peuvent être envisagées.Of course, different variants of the device as well described can be considered.

En premier lieu, on peut prévoir un laminage du métal à bas point de fusion 300 non point au niveau des interfaces définies entre la bague 150 et le piston 200 mais au niveau d'alésages calibrés formés dans la bague 150 ou dans le piston 200 délimitant la chambre 310.First, a low point metal rolling can be provided melting point 300 not at the interfaces defined between the ring 150 and the piston 200 but at the level of calibrated bores formed in the ring 150 or in the piston 200 delimiting the chamber 310.

En second lieu, comme on le décrira plus en détail par la suite, on peut envisager d'assurer la sollicitation en déplacement du piston 200, non point sous l'effet de gaz issus de la composition pyrotechnique 400, mais sous l'effet d'un organe de sollicitation auxiliaire, par exemple un élément ressort.Second, as will be described in more detail below, we may consider ensuring the displacement displacement of the piston 200, not point under the effect of gases from pyrotechnic composition 400, but under the effect of an auxiliary biasing member, for example an element spring.

Le métal à bas point de fusion 300 peut être thermiquement isolé de l'environnement extérieur afin d'éviter tout risque de fusion de ce métal 300 avant mise en oeuvre de la composition pyrotechnique 400.Low melting metal 300 can be thermally isolated from the external environment in order to avoid any risk of melting of this metal 300 before use of pyrotechnic composition 400.

A cet effet, de préférence, le corps 110 et le bouchon 130 disposés sur l'extérieur de la chambre 310 sont réalisés dans des matériaux présentant des propriétés de conduction thermique médiocre ou thermiquement isolantes, tandis que le piston 200 dont la paroi formant la section intermédiaire 216 est intercalée entre la composition pyrotechnique 400 et le métal à bas point de fusion 300 est réalisée de préférence en un matériau bon conducteur thermique.For this purpose, preferably, the body 110 and the plug 130 arranged on the outside of the chamber 310 are made of materials exhibiting poor heat conduction properties or thermally insulating, while the piston 200 whose wall forming the intermediate section 216 is inserted between the pyrotechnic composition 400 and the metal with a low melting point 300 is preferably produced in a material good thermal conductor.

Par ailleurs le métal 300 doit être choisi pour présenter une température de fusion ou de ramollissement supérieure à la température ambiante pour assurer sa fusion uniquement en cas de mise en oeuvre de l'initiateur 180.Furthermore, the metal 300 must be chosen to present a higher melting or softening temperature ambient to ensure its merger only in the event of implementation of initiator 180.

On va maintenant décrire la variante de réalisation illustrée sur la figure 2.We will now describe the embodiment illustrated on the figure 2.

On retrouve sur cette figure, une structure composée de deux ensembles 100, 200 susceptibles de translation relative selon un axe O-O, un métal à bas point de fusion 300 et une composition pyrotechnique 400.We find in this figure, a structure composed of two assemblies 100, 200 capable of relative translation along an axis O-O, a metal with a low melting point 300 and a pyrotechnic composition 400.

Au repos, le métal à bas point de fusion 300 assure une immobilisation entre les deux ensembles 100, 200. Lors de la mise en oeuvre de la composition pyrotechnique 400, le métal à bas point de fusion 300 est liquéfié et le gaz développé par la composition pyrotechnique 400 sollicite les ensembles 100, 200 à déplacement relatif. La structure est à nouveau immobilisée après refroidissement du métal 300. Par ailleurs, là encore, selon le mode de réalisation de la figure 2, le métal 300 est situé dans une chambre 310 définie entre, d'une part une bague 150 immobilisée entre un corps 110 et un bouchon 130, et d'autre part un piston 200. Plus précisément encore, la chambre 310 est délimitée par des éléments de la bague 150 et des éléments du piston 200, globalement en L possédant chacun un tronçon axial et un tronçon radial.At rest, the low-melting metal 300 provides a immobilization between the two assemblies 100, 200. When setting work of pyrotechnic composition 400, the metal with low melting point 300 is liquefied and the gas developed by the pyrotechnic composition 400 requests the sets 100, 200 with relative displacement. The structure is again immobilized after cooling of the metal 300. Furthermore, there again, according to the embodiment of Figure 2, the metal 300 is located in a chamber 310 defined between, on the one hand, a ring 150 immobilized between a body 110 and a plug 130, and on the other hand a piston 200. More again precisely, the chamber 310 is delimited by elements of the ring 150 and elements of the piston 200, generally in L having each an axial section and a radial section.

Cependant, le dispositif illustré sur la figure 2 présente par rapport à la figure 1 un certain nombre de points caractéristiques, parmi lesquels on peut citer les suivants.However, the device illustrated in FIG. 2 presents with respect to Figure 1 a number of characteristic points, among which we may cite the following.

Selon la figure 2, le piston 200 est formé d'une structure annulaire qui n'assure pas directement l'effet actionneur de sortie, mais contrôle l'élément de sortie.According to Figure 2, the piston 200 is formed of an annular structure which does not directly provide the actuator output effect, but controls the output element.

Plus précisément, cet élément de sortie est formé d'une structure 230 pouvant être formée par exemple d'un écrou, d'un système de pince constitué de différents segments, par exemple filetés équi-répartis autour de l'axe O-O, ou encore tout moyen équivalent. Cet élément formant actionneur de sortie 230 est emprisonné en position de repos initial entre deux troncs de cône 219, 139 formés respectivement sur le piston 200 et sur le bouchon 130.More precisely, this output element is formed of a structure 230 can be formed for example of a nut, a clamp system made up of different segments, for example threads equi-distributed around the O-O axis, or any equivalent means. This forming element output actuator 230 is trapped in the initial rest position between two truncated cones 219, 139 formed respectively on the piston 200 and on the cap 130.

Par ailleurs, le piston 200 est formé de deux pièces 202, 204 assemblées par filetage avec un joint 206 intercalé.Furthermore, the piston 200 is formed from two parts 202, 204 assembled by thread with an interposed seal 206.

Un joint torique 170 est placé dans une gorge 203 de la pièce 202 pour assurer l'étanchéité entre le piston 200 et le corps 110, de façon comparable à la figure 1.An O-ring 170 is placed in a groove 203 in the part 202 to seal between the piston 200 and the body 110, so comparable to Figure 1.

Un joint additionnel 172 placé dans une gorge 137 du bouchon 130 assure l'étanchéité entre ce dernier et le piston 200.An additional seal 172 placed in a groove 137 of the plug 130 seals between the latter and the piston 200.

L'initiateur 180 est placé dans un passage radial en regard de l'axe O-O traversant la paroi du corps 110. L'initiateur 180 débouche ainsi dans une chambre annulaire 140 contenant la composition pyrotechnique 400. Cette chambre 140 est délimitée radialement sur l'extérieur par la paroi interne du corps 110, axialement côté seconde extrémité du système par une surface transversale du piston 200 et axialement sur la première extrémité et radialement sur l'intérieur par la bague 150.The initiator 180 is placed in a radial passage opposite the axis O-O passing through the wall of the body 110. The initiator 180 thus opens into an annular chamber 140 containing the pyrotechnic composition 400. This chamber 140 is delimited radially on the outside by the wall internal of the body 110, axially on the second end of the system by a transverse surface of the piston 200 and axially on the first end and radially on the inside by the ring 150.

On notera par ailleurs qu'au niveau de la seconde extrémité, le corps 110 présente un flasque 1102 dirigé radialement vers l'intérieur et comportant un fourreau 1104 pourvu d'un taraudage 1106 interne. Un tel taraudage 1106 peut recevoir tout élément fileté complémentaire devant être maintenu provisoirement par rapport à un élément associé maintenu quant à lui par le taraudage 232 de l'élément central 230 formé d'un écrou ou d'une pince.Note also that at the second end, the body 110 has a flange 1102 directed radially inwards and comprising a sheath 1104 provided with an internal thread 1106. Such thread 1106 can receive any additional threaded element in front be temporarily maintained in relation to an associated associated element meanwhile by the thread 232 of the central element 230 formed of a nut or pliers.

Le dispositif illustré sur la figure 2 peut trouver application dans le relâchement contrôlé, lors de la mise en oeuvre de l'initiateur 180, d'un assemblage réalisé par des éléments filetés en prise respectivement avec les taraudages 1106 et 232.The device illustrated in FIG. 2 can find application in the controlled release, during the implementation of the initiator 180, of a assembly carried out by threaded elements engaged respectively with 1106 and 232 threads.

Là encore, l'initiation de la charge pyrotechnique 400 fortement exothermique, par l'initiateur électrique 180, permet la fusion du métal 300 à bas point de fusion, formant initialement une brasure entre la bague 150 et le piston 200, pour libérer le mouvement. Les gaz issus de la combustion et de la composition pyrotechnique 400 poussent le piston 200 vers la seconde extrémité de la structure. Le métal liquide 400 est alors laminé dans le jeu des ajustements formés entre le piston 200 et la bague 150, pour former une fonction amortisseur contrôlant la dynamique du piston.Again, the initiation of the pyrotechnic charge 400 strongly exothermic, by the electric initiator 180, allows the metal 300 to melt low melting point, initially forming a solder between the ring 150 and the piston 200, to release the movement. The gases from combustion and of the pyrotechnic composition 400 push the piston 200 towards the second end of the structure. The liquid metal 400 is then laminated in the set of adjustments formed between the piston 200 and the ring 150, to form a damping function controlling the dynamics of the piston.

On va maintenant décrire la variante de réalisation illustrée sur la figure 3 annexée.We will now describe the embodiment illustrated on the Figure 3 attached.

On retrouve dans cette variante une structure comprenant deux ensembles 100, 200 susceptibles de déplacement relatif, mais immobilisés initialement par un métal à bas point de fusion 300 formant brasure, entre une bague 150 liée au premier ensemble et le second ensemble 200 formant piston, ainsi qu'une composition pyrotechnique fortement exothermique 400 associée à un initiateur électrique 180.We find in this variant a structure comprising two sets 100, 200 susceptible of relative displacement, but immobilized initially by a metal with a low melting point 300 forming a solder, between a ring 150 linked to the first set and the second set 200 forming a piston, as well as a highly pyrotechnic composition exothermic 400 associated with an electric initiator 180.

Par ailleurs, là encore, le premier ensemble 100 est formé par assemblage d'un corps 110 et d'un bouchon 130. Furthermore, here again, the first set 100 is formed by assembly of a body 110 and a plug 130.

L'initiateur pyrotechnique 180 est placé dans un canal radial traversant la paroi du corps externe 110 et débouche dans une chambre annulaire 140 délimitée par le corps 110, la bague 150, et dans sa portion radialement interne par la périphérie externe du piston 200.The pyrotechnic initiator 180 is placed in a radial channel passing through the wall of the external body 110 and opens into a chamber annular 140 delimited by the body 110, the ring 150, and in its portion radially internal by the external periphery of the piston 200.

La bague 150 est également liée au premier ensemble 100. Elle possède pour cela une portion pincée entre un épaulement du corps 110 et le bouchon 130.The ring 150 is also linked to the first set 100. It has for this a pinched portion between a shoulder of the body 110 and the cap 130.

La chambre annulaire 310 qui contient le métal à bas point de fusion 300 formant brasure, située radialement sur l'intérieur de la chambre 140 et contenant la composition pyrotechnique 400 est délimitée par deux paires de parois en L appartenant respectivement à la bague 150 et au piston 200, chacune de ces deux paires de parois possédant une paroi 154, 218 d'orientation radiale transversale à l'axe O-O et une paroi 152, 216 d'orientation axiale parallèle à l'axe O-O.The annular chamber 310 which contains the metal at low point fusion 300 forming solder, located radially on the inside of the chamber 140 and containing the pyrotechnic composition 400 is delimited by two pairs of L-shaped walls belonging respectively to the ring 150 and to the piston 200, each of these two pairs of walls having a wall 154, 218 of radial orientation transverse to the axis O-O and a wall 152, 216 axial orientation parallel to the O-O axis.

Selon la figure 3, la chambre 140 contenant la composition pyrotechnique 400 n'étant délimitée que radialement sur l'intérieur par le piston 200, l'on comprend que les gaz éventuellement générés par la composition pyrotechnique 400 ne peuvent solliciter la structure en déplacement.According to FIG. 3, the chamber 140 containing the composition pyrotechnic 400 being delimited only radially on the inside by the piston 200, it is understood that the gases possibly generated by the pyrotechnic composition 400 cannot stress the structure in displacement.

Dans ce contexte, selon la figure 3, le piston 200 est sollicité à déplacement vers la seconde extrémité de la structure, après fusion de la brasure 300 par un élément de sollicitation auxiliaire, par exemple un ressort. En variante, le piston 200 peut être sollicité par un élément extérieur à la structure illustrée sur la figure 3, par exemple une sangle sollicitant le piston 200 à la traction vers l'extérieur du corps 110.In this context, according to FIG. 3, the piston 200 is stressed at displacement towards the second end of the structure, after fusion of the solder 300 by an auxiliary biasing element, for example a spring. As a variant, the piston 200 can be stressed by an element outside the structure illustrated in FIG. 3, for example a strap biasing the piston 200 towards the outside of the body 110.

Comme on l'a évoqué précédemment, le mode de réalisation illustré sur la figure 3 permet entre autres de provoquer un relâchement entre les pièces tendues tel que des sangles, câbles, etc ...As mentioned above, the illustrated embodiment in FIG. 3 makes it possible inter alia to cause a relaxation between the tensioned parts such as straps, cables, etc ...

On va maintenant décrire la variante de réalisation illustrée sur la figure 4.We will now describe the embodiment illustrated on the figure 4.

Celle-ci reprend les dispositions générales illustrées sur la figure 1 et précédemment décrites. Elle se distingue cependant du mode de réalisation précédemment décrit en regard de la figure 1 par le fait que selon la figure 4, la structure comprend deux compositions pyrotechniques 400, 410 reliées entre elles par un relais pyrotechnique 420.This repeats the general provisions illustrated in Figure 1 and previously described. However, it differs from the embodiment previously described with reference to FIG. 1 by the fact that according to FIG. 4, the structure comprises two pyrotechnic compositions 400, 410 linked together by a pyrotechnic relay 420.

La première composition pyrotechnique 400 communique avec l'initiateur électrique 180. Elle est placée dans une chambre annulaire 220 formée dans le piston 200 à proximité du métal 300, plus précisément radialement sur l'intérieur de la chambre 310 délimitée par la bague 150 et la périphérie externe du piston 200.The first pyrotechnic composition 400 communicates with the electric initiator 180. It is placed in an annular chamber 220 formed in the piston 200 near the metal 300, more precisely radially on the inside of the chamber 310 delimited by the ring 150 and the outer periphery of the piston 200.

Cette première composition pyrotechnique 400 est fortement exothermique mais peut le cas échéant générer peu de gaz. Elle a pour fonction de faire fondre le métal 300 adjacent.This first pyrotechnic composition 400 is strongly exothermic but can generate little gas if necessary. She has for function of melting the adjacent metal 300.

La seconde composition pyrotechnique 410 est placée dans une chambre borgne 222 ménagée en position centrale dans le piston 200 et débouchant sur la première extrémité de la structure côté bouchon obturateur 130. Le retard pyrotechnique 420 est placé dans un passage radial reliant les deux chambres 220, 222. Ainsi la seconde composition pyrotechnique 410 est mise en oeuvre après la première composition pyrotechnique 400, selon un retard défini par la combustion du retard pyrotechnique 420. La seconde composition pyrotechnique 410 est conçue pour générer un volume de gaz suffisant pour déplacer le piston 200 comme décrit précédemment en regard de la figure 1.The second pyrotechnic composition 410 is placed in a blind chamber 222 formed in a central position in the piston 200 and leading to the first end of the cap side structure shutter 130. The pyrotechnic delay 420 is placed in a passage radial connecting the two chambers 220, 222. Thus the second composition pyrotechnic 410 is implemented after the first composition pyrotechnic 400, according to a delay defined by the combustion of the delay pyrotechnic 420. The second pyrotechnic composition 410 is designed to generate a sufficient volume of gas to move the piston 200 as previously described with reference to FIG. 1.

L'utilisation de deux compositions pyrotechniques 400, 410 destinées à assurer respectivement la fusion du métal 300 et le déplacement du piston 200 permet un contrôle séquentiel précis des fonctionnements de la structure.The use of two pyrotechnic compositions 400, 410 intended to ensure respectively the fusion of the metal 300 and the displacement of piston 200 allows precise sequential control of functioning of the structure.

On va maintenant décrire la variante de réalisation illustrée sur la figure 5.We will now describe the embodiment illustrated on the figure 5.

Cette variante reprend également les concepts généraux illustrés sur la figure 1 et décrits précédemment. Par ailleurs, la variante de réalisation illustrée sur la figure 5 comprend également deux compositions pyrotechniques 400, 410 destinées à assurer respectivement la fusion du métal 300 et la génération de gaz propre à déplacer le piston 200. Cependant, contrairement à la figure 4, les deux compositions pyrotechniques 400, 410 ne sont pas reliées par un retard pyrotechnique. Elles sont au contraire associées à des initiateurs, par exemple électriques, respectifs, 180, 182 portés par le bouchon 130. Dans ce cas, le séquencement n'est pas contrôlé par effet pyrotechnique dû à un retard comme décrit pour la figure 4, mais par l'application de signaux appropriés sur les initiateurs respectifs 180, 182.This variant also incorporates the general concepts illustrated in Figure 1 and described above. Furthermore, the variant of embodiment illustrated in Figure 5 also includes two compositions pyrotechnics 400, 410 intended respectively to ensure the fusion of metal 300 and the generation of clean gas to move the piston 200. However, unlike Figure 4, the two compositions pyrotechnics 400, 410 are not connected by a pyrotechnic delay. On the contrary, they are associated with initiators, for example electrical, respective, 180, 182 carried by the plug 130. In this case, the sequencing is not controlled by pyrotechnic effect due to a delay as described for figure 4, but by applying appropriate signals on the respective initiators 180, 182.

Par ailleurs, selon la figure 5, de façon comparable à la figure 4, la première composition pyrotechnique 180 fortement exothermique est située en position adjacente au métal 300, dans une chambre annulaire du piston 200, tandis que la seconde composition pyrotechnique 410, génératrice de gaz, est située dans une chambre centrale borgne 222 du piston 200.Furthermore, according to FIG. 5, in a manner comparable to FIG. 4, the first pyrotechnic composition 180 highly exothermic is located adjacent to metal 300, in an annular piston chamber 200, while the second pyrotechnic composition 410, generating gas, is located in a blind central chamber 222 of the piston 200.

Bien entendu la présente invention n'est pas limitée aux modes de réalisation particuliers qui viennent d'être décrits.Of course, the present invention is not limited to the modes of particular realization which have just been described.

En particulier alors que selon les modes de réalisation précédemment décrits, le dispositif conforme à la présente invention constitue essentiellement un actionnement à déplacement linéaire selon l'axe O-O du dispositif en variante, on peut prévoir que celui-ci génère des efforts transversaux à l'axe O-O, par exemple de pince par resserrement de segments d'orientation générale axiale équi-répartis autour de l'axe O-O, grâce à des moyens, en coin ou en cône liés au piston 200 déplacé.In particular while according to the embodiments previously described, the device according to the present invention essentially constitutes a linear displacement actuation according to the O-O axis of the device as a variant, provision can be made for the latter to generate forces transverse to the axis O-O, for example of clamp by tightening of segments of general axial orientation equi-distributed around the axis O-O, by means, in a corner or in a cone linked to the displaced piston 200.

A titre d'exemple non limitatif le métal 300 à bas point de fusion peut être formé de :

  • Bi50/Pb28/Sn22 (pour une température de fusion de l'ordre de 95-110°C) ou
  • In (pour une température de fusion de l'ordre de 156°C) ou
  • Sn ou Sn85/Zn15 (pour une température de fusion de l'ordre de 200-250°C) ou
  • Pb82,5/Cd17,5 ou
  • Pb96/Sb4 (pour une température de fusion de l'ordre de 250-300°C),
tandis que la composition pyrotechnique 400 peut être formée de :
  • Al + Fe2O3 ou
  • Mg + Fe2O3 ou
  • Al + CuO ou
  • Mg + CuO.
By way of nonlimiting example, the metal 300 with a low melting point can be formed from:
  • Bi50 / Pb28 / Sn22 (for a melting temperature of the order of 95-110 ° C) or
  • In (for a melting temperature of the order of 156 ° C) or
  • Sn or Sn85 / Zn15 (for a melting temperature of the order of 200-250 ° C) or
  • Pb82.5 / Cd17.5 or
  • Pb96 / Sb4 (for a melting temperature of the order of 250-300 ° C),
while the pyrotechnic composition 400 can be formed from:
  • Al + Fe 2 O 3 or
  • Mg + Fe 2 O 3 or
  • Al + CuO or
  • Mg + CuO.

Par ailleurs dans le cadre de la présente invention :

  • le métal 300 à bas point de fusion peut être remplacé par tout matériau approprié, par exemple paraffine, alliages eutectiques, etc...
Furthermore, in the context of the present invention:
  • metal 300 with a low melting point can be replaced by any suitable material, for example paraffin, eutectic alloys, etc.

Claims (24)

  1. A mechanism-forming device, in particular for application in space, the device comprising in combination:
    a low melting point material (300);
    at least one heater means (400); and
    means suitable for throttling the low melting point material (300) in the liquid state, after the heater means (400) have operated, thereby performing a shock-absorbing function, the device being characterized by the fact that the heater means (400) comprise at least one highly exothermal pyrotechnical composition.
  2. A device according to claim 1, characterized that the fact that the low melting point metal (300) is adapted to perform soldering, and by the fact that the device further comprises a structure presenting architecture that possesses a zone that is blocked by the low melting point metal (300) and that is capable of being released by the low melting point material liquefying when the heater means are operated.
  3. A device according to claim 1 or claim 2, characterized by the fact that it comprises at least two concentric surfaces (154, 216; 152, 218) provided respectively on parts (150, 200) that are capable of moving in order to throttle the low melting point material (300).
  4. A device according to claim 1 or claim 2, characterized by the fact that it has at least one calibrated bore opening out into the chamber containing the low melting point material (300) for throttling purposes.
  5. A device according to any one of claims 1 to 4, characterized by the fact that the pyrotechnical composition (400, 410) is designed to generate a volume of gas that is sufficient to drive relative displacement of the two parts (100, 200) of the device.
  6. A device according to any one of claims 1 to 5, characterized by the fact that it has an external element, such as a resilient member of an element working in traction, suitable for driving relative displacement between the two parts (100, 200) of the device after the heater means (400) have been operated.
  7. A device according to any one of claims 1 to 6, characterized by the fact that the low melting point material (300) is situated in a chamber (310) designed to be reduced in volume during operation of the heater means (400).
  8. A device according to any one of claims 1 to 7, characterized by the fact that the chamber (310) housing the melting point material (300) is defined by two L-shaped structures, each possessing both an axially-extending wall (152,216) and a radially-extending wall (254, 218) secured respectively to two assemblies (100, 200) capable of relative movement.
  9. A device according to claim 8, characterized by the fact that the chamber (310) housing the melting point material (300) is defined at least in part by a ring (150) secured to a fixed body (110).
  10. A device according to claim 9, characterized by the fact that the ring (150) is clamped between an outer shell body (110) and a closure plug (130).
  11. A device according to any one of claims 1 to 10, characterized by the fact that the chamber (310) housing the melting point material (300) is thermally insulated from the external environment.
  12. A device according to any one of claims 1 to 11, characterized by the fact that it comprises an outer shell body (110) that is thermally insulating.
  13. A device according to any one of claims 1 to 12, characterized by the fact that it includes a piston (200) suitable for being moved out from a shell body after the heater means (200) have been operated, thereby forming a linear actuator.
  14. A device according to any one of claims 1 to 13, characterized by the fact that it has two parts (100, 230) capable of relative movement for releasing an assembly when the heater means are operated.
  15. A device according to any one of claims 1 to 14, characterized by the fact that it includes a nut (230) suitable for being released when the heater means are operated.
  16. A device according to any one of claims 1 to 15, characterized by the fact that it has a nut (230) made up of a plurality of segments uniformly distributed around an axis and suitable for being released when the heater means are operated.
  17. A device according to any one of claims 1 to 16, characterized by the fact that it includes a clamp structure constituted by a plurality of general axially extending segments (194) uniformly distributed around an axis O-O and suitable for moving towards one another during displacement of a piston (200) having an actuator surface in the form of a truncated cone, after the heater means (400) have been operated.
  18. A device according to any one of claims 1 to 17, characterized by the fact that it includes an initiator (180) associated with the heater means (400).
  19. A device according to any one of claims 1 to 18, characterized by the fact that the heater means comprises two pyrotechnical compositions (400, 410), respectively one composition that is highly exothermal and another composition that generates gas, thereby respectively melting the low melting point material (300) and driving the structure.
  20. A device according to claim 19, characterized by the fact that the two pyrotechnical compositions (400, 410) communicate via a pyrotechnical delay (420).
  21. A device according to claim 19, characterized by the fact that the two pyrotechnical compositions (400, 410) are actuated by respective initiators (180, 182).
  22. A device according to any one of claims 1 to 21, characterized by the fact that the mechanism constitutes a pyromechanism.
  23. A device according to any one of claims 1 to 22, characterized by the fact that the low melting point material is a metal (300).
  24. A device according to any one of claims 1 to 23, characterized by the fact that the low melting point material (300) is selected from the group comprising paraffin and eutectic alloys.
EP00971506A 1999-11-30 2000-10-25 Shockproof mechanism, in particular for use in space sector Expired - Lifetime EP1234117B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR9915178 1999-11-30
FR9915178A FR2801649B1 (en) 1999-11-30 1999-11-30 PYROMECANISM, ESPECIALLY FOR SPATIAL APPLICATION
PCT/FR2000/002976 WO2001040664A1 (en) 1999-11-30 2000-10-25 Shockproof mechanism, in particular for use in space sector

Publications (2)

Publication Number Publication Date
EP1234117A1 EP1234117A1 (en) 2002-08-28
EP1234117B1 true EP1234117B1 (en) 2003-05-14

Family

ID=9552788

Family Applications (1)

Application Number Title Priority Date Filing Date
EP00971506A Expired - Lifetime EP1234117B1 (en) 1999-11-30 2000-10-25 Shockproof mechanism, in particular for use in space sector

Country Status (9)

Country Link
US (1) US6755020B1 (en)
EP (1) EP1234117B1 (en)
JP (1) JP2003515500A (en)
CN (1) CN1300476C (en)
AT (1) ATE240461T1 (en)
AU (1) AU1035001A (en)
DE (1) DE60002756T2 (en)
FR (1) FR2801649B1 (en)
WO (1) WO2001040664A1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2806788B1 (en) * 2000-03-24 2002-12-06 Lacroix Soc E PYROMECANISM, ESPECIALLY FOR APPLICATION IN THE SPACE AREA
FR2825766B1 (en) * 2001-06-08 2003-10-10 Lacroix Soc E THERMAL EFFECT CONTROLLED RELEASE MECHANISM
FR3009283B1 (en) * 2013-08-01 2017-06-09 Astrium Sas METHOD AND DEVICE FOR BONDING AND SEPARATING TWO ELEMENTS WITH BINDING PLATES

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2857890A (en) * 1957-10-07 1958-10-28 Albert M Stott Thruster with damper
GB2004984B (en) * 1977-09-27 1982-03-17 Secr Defence Piston and cylinder arrangements
DE3238710C2 (en) * 1982-10-19 1986-10-23 TRW Repa GmbH, 7077 Alfdorf Drive device with a piston driven pyrotechnically in a cylinder
US4842106A (en) * 1987-10-08 1989-06-27 Hughes Aircraft Company Rate controllable damping mechanism
DE9400764U1 (en) * 1994-01-18 1994-02-24 Trw Repa Gmbh, 73553 Alfdorf Piston safety catch for a pyrotechnic piston / cylinder linear drive
US5639120A (en) * 1995-09-27 1997-06-17 Ford Motor Company Seat belt buckle pretensioner with end cap

Also Published As

Publication number Publication date
CN1300476C (en) 2007-02-14
FR2801649A1 (en) 2001-06-01
JP2003515500A (en) 2003-05-07
ATE240461T1 (en) 2003-05-15
CN1413294A (en) 2003-04-23
DE60002756T2 (en) 2004-02-19
AU1035001A (en) 2001-06-12
FR2801649B1 (en) 2002-02-15
WO2001040664A1 (en) 2001-06-07
DE60002756D1 (en) 2003-06-18
EP1234117A1 (en) 2002-08-28
US6755020B1 (en) 2004-06-29

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